Accession Number:

AD0256172

Title:

PROPOSED INVESTIGATION OF VISCOUS-INVISCID EFFECTS IN HYPERSONIC FLOW IN THE AEDC GAS DYNAMICS FACILITY TUNNEL B. PHASE II

Descriptive Note:

Technical memo.

Corporate Author:

GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y

Personal Author(s):

Report Date:

1960-03-28

Pagination or Media Count:

1.0

Abstract:

A test program is presented for a series of hypersonic research tests to provide detailed data for pressure distribution and heat transfer over several model configurations. The model configurations include delta planforms 70 degrees lambda 0 degrees dihedral, 70 degrees lambda 10 degrees cathedal, 70 degrees lambda 10 degrees dihedral, 60 degrees lambda 0 degrees dihedral, 75 degrees lambda 0 degrees dihedral, fin-flat plate interference 90 degrees Fin, and 45 degrees fin-flat plate interference.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE